Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = '1900D' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = '1900D' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR GLBA2013112200351Handle · separatedPILOT REPORTED THAT THE AIR STAIR DOOR HANDLE CAME OFF. INSTALLED A NEW SNAP RING & REINSTALLED DOOR HANDLE, IAW BMM 52-10-05, OPS CHECKED GOOD.SDR GLBA2013112100350Terminal · out of positionPILOT REPORTED THAT SPARKS WERE COMING OUT FROM BEHIND THE ICE PROTECTION PANEL. THE RT PITOT TERMINAL CONTACTING THE MOUNTING STRUCTURE REPOSITIONS THE RT PITOT TERMINAL END FOR CLEARANCE, ALL CHECKED GOOD.SDR CA131202001Engine · malfunctioned(CAN) SHORTLY AFTER THE TAKEOFF, THE RT ENGINE TORQUE INCREASED TO 4500 LB AND THE PROPELLER RPM DROPPED TO 500. THE PILOT IN CHARGE IMMEDIATELY REDUCED THE THROTTLE, WHICH BROUGHT DOWN THE ENGINE TORQUE, TORQUE INCREASE WAS WITHIN MM LIMITS, THE PROPELLER RPSDR CA131107003Tube · melted(CAN) CREW SNAGGED TAIL DE-ICE ANNUNCIATOR NOT ILLUMINATING. UPON INSPECTION FOUND DAMAGE TO THE LT HORIZONTAL STABILIZER TAILET PNEUMATIC DE-ICE SUPPLY TUBE. DAMAGE WAS DIRECTLY ABOVE THE LT LOGO LIGHT ASSY, AND THE DAMAGE APPEARS TO BE DUE TO EXCESSIVE HEASDR GLBA2013110100347Skin · damagedDURING A SCHEDULED INSPECTION, FOUND A DENT FROM A BIRD STRIKE ON THE LT WING L/E BETWEEN WS 236.62 AND 223.48 AND HAS A FUEL LEAK DUE TO THE DAMAGE. REPAIRED IAW EO 13-1900-57-019. MAJOR REPAIRSDR CA131101004Shaft · sheared(CAN) ON CLIMBOUT, CREW SELECTED FLAPS UP AND NOTICED THAT THEY DID NOT RETRACT, FLIGHT SERVICES WERE NOTIFIED THAT THEY WERE RETURNING TO THE AIRPORT. MAINTENANCE INSPECTED THE SYS AND FOUND THAT THE SPLIT FLAP SYS HAD ACTIVATED. SPLIT FLAP BY PASS SWITCH WSDR GLBA2013103000346Door Frame · crackedDURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE AFT LOWER CARGO DOOR FRAME AT FS 509.50 AND BETWEEN STRINGERS 10 - 11L, 2.5 INCHES IN LENGTH. REPAIRED IAW EO 13-1900-53-077.SDR CA131122003Skin · corroded(CAN) DURING REPLACEMENT OF LT WING DEICE BOOT, UNDER BOOT FOUND PITTING CORROSION OF WING SKIN. CORROSION FOUND TO BE FROM .003-.021 DEEP.SDR GLBA2013102300344Stringer · corrodedDURING A SCHEDULED INSPECTION FOUND CORROSION ON STRINGER 16 AT FS 243.25, RUNS APPROX 6 INCHES. REPAIRED IAW EO 13-1900-53-075. MAJOR REPAIR.SDR GLBA2013102200343Skin · corrodedDURING A SCHEDULED INSPECTION, FOUND BELLY SKIN CORRODED AT FS 243.25 AND STRINGER 16. REPAIRED IAW EO 13-1900-53-076. MAJOR REPAIR.SDR GLBA2013102200342Indicator · malfunctionedPILOT REPORTED AFTER TAKE OFF, LT PROP RPM ROSE TO 1730 FOR 15 SECS, PULLED BACK PROP LEVERS AND CONTINUED TO CLIMB, LEVELED OFF AND TRIED TO SYNC PROPS, RECEIVED A VIBRATION, TURNED OFF PROP SYNC AND SYNC'D, NR 1 AT 1400 AND NR 2 AT 1550, STARTED LOSING PROPSDR GLBA2013102100341Seal · unsecurePILOT REPORTED THAT THE CABIN ALT HI ILLUM AT FLT LEVEL 240, CABIN ALT STARTED CLIMBING TO AC ALT, O2 MASKS DEPLOYED. MAINTENANCE RESECURED AIRSTAIR DOOR SEAL, OPS CK GOOD.SDR GLBA2013101400339Engine · making metalDURING DESCENT, TORQUE ON NR 2 ENGINE DECREASED TO APPROX 400 LBS AND ITT INCREASED TO ABOVE 800 CELSIUS F/O SAW FLAMES COMING OUT BOTH EXHAUST STACKS ON NR 2 ENGINE. SECURED ENGINE USING APPROPRIATE CHECKLISTS. MAINTENANCE FOUND PROPELLER STIFF. FOUND DAMASDR GLBA2013101400340Circuit Breaker · failedPILOT REPORTED THAT THE LT AUTOFEATHER SYS WILL NOT ENGAGE, THE AUTOFEATHER LIGHT IS NOT ILLUMINATED, BUT DOES PRESS TO TEST. MAINTENANCE REPLACED PCB A129, PERFORMED RUN, OPS CK GOOD.SDR 29GA2013101494253Skin · corrodedREWORK PREVIOUS SKIN REPAIR AT FS 255 AT RINGER 14L AS DIRECTED. REPAIRED DAMAGE USING COVER PATCH METHOD, REPLACED EXISING PATCH REPAIR INSTALLED 9.5 X 11.00 INSERT AND 13.0 X 13.75 EXTERNAL DOUBLER.SDR CA131018002Switch · stuck(CAN) ON DESCENT THROUGH APPROXIMATELY 12,000 FEET, CAPTAIN NOTICED A LOSS OF VOLUME IN HIS HEADSET. PILOTS CHECKED CONNECTIONS, VOLUME SETTINGS FOUND NOTHING. CREW WAS ABLE TO HEAR ATC, THEY WERE REPORTING TO ALL ACFT THAT SOMEONE HAD A STUCK MIC, FURTHER INSDR 29GA2013101095432Circuit Breaker · trippedLANDING GEAR INDICATOR CIRCUIT BREAKER TRIPPED AFTER TAKEOFF. RETURNED AND LANDED SAFELY. INSPECTED WIRING FROM CIRCUIT BREAKER TO HANDLE, OPS CHECKED NUMEROUS TIMES, OPS CHECKED GOOD.SDR 29GA2013101195432Annunciator · false activationLOWER LT RED ANNUNCIATOR AND YELLOW MASTER CAUTION COMES ON WITH GEAR RED LIGHT IN FLIGHT. PERFORMED DETAILED OPS CHECK OF LANDING GEAR OPS CHECKED GOOD.SDR GLBA2013100800338Propeller · making metalPILOT REPORTED THAT THE RT PROP FEATHERED ON FINAL, BEFORE PROPS PUSHED FWD, PROPS AT 1550 TORQUE, DID NOT SECURE ENGINE, PULLED POWER BACK TO IDLE, AS 180KTS, FLAPS 17, DECLARED AN EMERGENCY, SECURED ENGINE ONCE ON GROUND. MAINTENANCE FOUND PROPELLER STIFF ASDR GLBA2013100800336Bulb · inoperativePILOT REPORTED THAT THE EMERGENCY LIGHT AT ROW 6 IS INOPERAITVE. MAINTENANCE REPLACED BULB, OPS CHECKED GOOD.SDR GLBA201310080336Propeller · malfunctionedPILOT REPORTED THAT ON SHORT FINAL THE RT PROP FEATHERED, BEFORE PROPS PUSHED FWD, PROPS AT 1550 TQ 1500, DID NOT SECURE ENG, PULLED PWR BACK TO IDLE, A/S 180 KTS, FLAPS 17, DECLARED EMERGENCY, SECURED ENG ON GROUND, 10 MINS FROM DEPT HAD TQ/PROP FLUX +-25RPMSDR GLBA2013100800337Skin · dentedDURING A SCHEDULED INSPECTION FOUND A DENT AFTER A BIRD STRIKE TO THE RIGHT WING AT WS 264.74 AND 283.74, 19" LONG X 1.75" DEEP. REPAIRED AREA IAW EO 13-1900-57-018. MAJOR REPAIR.SDR GLBA2013100400335Structure · crackedDURING A SCHEDULED INSPECTION, FOUND CRACK IN THE HORIZONTAL STABILIZER LT LOWER TEE SECTION AT HSS 0.00, .5" IN LENGTH. REPAIRED IAW EO 13-1900-55-024.SDR GLBA2013100200332Frame · crackedDURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE FUSELAGE FRAME ANGLE IN THE BEND RADIUS AT FS 451 AND STRINGER 10R, .875 INCH IN LENGTH. REPAIRED IAW EO 13-1900-53-068. MAJOR REPAIR.SDR GLBA2013100200330Frame · crackedDURING A SCHEDULED INSPECTION FOUND A CRACK BS 107 AND STRINGER 8R FRAME, 0.5 INCH IN LENGTH. REPAIRED IAW EO 13-1900-53-070. MAJOR REPAIR.SDR GLBA2013100200331Frame · crackedDURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE FRAME LT SIDE OF FS 107 BY STRINGER 8L, .125 INCH IN LENGTH. REPAIRED IAW EO 13-1900-53-069. MAJOR REPAIR.SDR GLBA2013100200333Frame · crackedDURING A SCHEDULED INSPECTION FOUND TWO CRACKS IN FUSELAGE FRAME, STRINGER 8L BS 438.25, .999 INCH IN LENGTH. REPAIRED IAW EO 13-1900-53-067. MAJOR REPAIR.SDR GLBA2013100200329Skin · crackedDURING A SCHEDULED INSPECTION, FOUND TWO CRACKS IN FUSELAGE SKIN, PROTRUDING OUT OF 2 RIVETS AT FS 150.6 STRINGER 1, 0.5 INCH IN LENGTH. REPAIRED IAW EO 13-1900-53-071. MAJOR REPAIR.SDR GLBA2013100200328Frame · crackedDURING A SCHEDULED INSPECTION, FOUND TWO CRACKS IN THE FUSELAGE FRAME ON EITHER SIDE OF STRINGER 2L AT FS 378.25, ONE INCH IN LENGTH. REPAIRED IAW EO 13-1900-53-072. MAJOR REPAIR.SDR GLBA2013100200327Spar Cap · crackedDURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE RT FWD SPAR CAP ANGLE ON THE VERTICAL STAB 2ND FROM TOP RIVET, .125 INCHES IN LENGTH. REPAIRED IAW EO 13-1900-55-023. MAJOR REPAIR.SDR GLBA2013100200326Structure · crackedDURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE EXIT DOOR 4C, UPPER FWD CORNER, 1.5 INCHES IN LENGTH. REPAIRED IAW EO 13-1900-52-002. MAJOR REPAIR.SDR GLBA2013092600325Structure · damagedDURING A SCHEDULED INSPECTION, FOUND DAMAGE ON THE BOTTOM SIDE OF THE WING TIP, APPROXIMENTLY 3 INCHES FROM WING TIP, DAMAGE DOES NOT APPEAR TO PENATRATE HONEYCOMB. REPLACED THE LT WING TIP ASSY IAW 57-30-00. MAJOR REPAIR.SDR 29GA94252092613APushrod · brokenAIRSTAIR DOOR HANDLE PUSHROD BROKEN UPON CLOSING THE DOOR. REPLACED CREW DOOR HANDLE LINK ASSY.SDR 2013FA0000580Handle · brokenAIRSTAIR DOOR HANDLE PUSHROD BROKEN UPON CLOSING THE DOOR. REPLACED CREW DOOR HANDLE LINK ASSY.SDR GLBA2013092600324Wire Harness · damagedPILOT REPORTED THAT WITH ANTI-SKID ON BRAKES TOTALLY INOPERATIVE. BRAKES WORK NORNALLY WITH ANTI-SKID OFF. FOUND LT TRANSDUCER HARMESS DAMAGED. R & R WIRE HARNESS AND TRANSDUCER CONNECTIONS IAW AIM 14 PARA 14.3.9 OPS CHECKED GOOD.SDR CA130923008Actuator · cracked(CAN) DURING FLAP SYSTEM TROUBLESHOOTING A CRACK WAS IDENTIFIED ON THE THREADED BORE OF THE RT OTBD FLAP ACTUATOR AT THE STAKING PIN LOCATION.SDR GLBA2013092000322Frame · crackedDURING A SCHEDULED INSP FOUND A CRACK IN THE FUSELAGE FRAME DOUBLER AT BS 177.35 AND STRINGER 13L 1.2 INCHES FROM OTBD EDGE RADIATING INBD, CRACK IS IN THE FLANGE BEND RADIUS OF THE DOUBLER. REPAIRED IAW EO 13-1900-53-064. MAJOR REPAIR.SDR GLBA2013092000321Frame · crackedDURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE FUSELAGE FRAME AT BS 177.35 AND STRINGER 13L AT THE FRAME FLANGE BEND RADIUS 1.2 INCHES FROM THE OTBD EDGE RADIATING INBD. REPAIRED IAW EO 13-1900-53-065. MAJOR REPAIR.SDR GLBA2013092000320Bulkhead · chafedDURING A SCHEDULED INSPECTION, FOUND A CHAFE IN THE LT WING TO FUSELAGE BULKHEAD AT STRINGER 12L BETWEEN BS 258.25 - 273.25, AREA OF BULKHEAD THAT MEETS AT BELLY SKIN EDGE. REPAIRED IAW EO 13-1900-53-066. MAJOR REPAIR.SDR GLBA2013091900318Door Frame · crackedDURING A SCHEDULED INSPECTION, MX FOUND THE CARGO DOOR FWD FRAME AT FS 456 CRACKED AT THE UPPER INBD GAS STRUT MOUNT ATTACHING NUT PLATE. THE CRACKS RADIATE UPWARD AND INBD FROM THE NUT PLATE. REPAIRED IAW EO 13-1900-53-074. MAJOR REPAIR.SDR GLBA2013091900319Frame · crackedDURING A SCHEDULED INSPECTION, MX FOUND THE RT SIDEWALL AT FS 164.415 & STRINGER 9AR, FRAME CUTOUT FOR STRINGER CRACKED .25". REPAIRED IAW EO 13-1900-53-063. MAJOR REPAIR.SDR GLBA2013091900316Spar Cap · crackedDURING A SCHEDULED INSPECTION, MX FOUND THE LT FWD SPAR CAP ON THE VERTICAL STABILIZER CRACKED AT THE SECOND HOLE. THE CRACK IS APPROXIMATELY .1250 INCHES IN LENGTH. REPAIRED IAW EO 13-1900-55-020. MAJOR REPAIR.SDR GLBA2013091900315Spar Cap · crackedDURING A SCHEDULED INSPECTION, MX FOUND THE RT FWD SPAR CAP ON THE VERTICAL STABILIZER CRACKED AT THE THIRD HOLE. THE CRACK IS APPROXIMATELY .1250" IN LENGTH. REPAIRED IAW EO 13-1900-55-021. MAJOR REPAIR.SDR GLBA2013091900314Spar · crackedDURING A SCHEDULED INSPECTION, MX FOUND THE AFT MIDDLE SPAR WEB ON THE HORIZONTAL STABILIZER CRACKED. REPAIRED IAW EO 13-1900-55-022. MAJOR REPAIR.SDR GLBA2013091900313Rib · crackedDURING A SCHEDULED INSPECTION, MX NOTED THAT THE RT WING INBD RIB FLANGE AND DOUBLER WERE CRACKED. REPAIRED IAW EO 13-1900-57-016. MAJOR REPAIR.SDR GLBA2013091900317Door Frame · crackedDURING A SCHEDULED INSPECTION, MX FOUND THAT THE AIRSTAIR DOOR LOWER AFT FRAME CORNER AREA AT APPROXIMATELY FS 172.35 WAS CRACKED, 1.2" IN THE OTBD UPPER BEND RADIUS. REPAIRED IAW EO 13-1900-53-061. MAJOR REPAIR.SDR CA130921002Oil System · low pressure(CAN) THIS EVENT WAS INDUCED IN CRM AFTER INVESTIGATION REPORT. THE ACFT WAS AT 15,000 FEET, THE RT ENGINE LOW OIL PRESSURE WARNING LIGHT ILLUMINATED. THE CREW CHECKED THE OIL PRESSURE GAUGE AND CONFIRMED THE INDICATION WAS BELOW 60 PSI. A LIGHT VIBRATION WSDR GLBA2013091600311Keelbeam · bentLT INBD KEEL WEB ASSY APPEARS BENT, FWD UPPER EDGE OF WEB ASSY APPEARS TO BE DEFLECTED OTBD APPROXIMATELY .125". LOCATION BL 91.75. REPAIRED IAW EO 13-1900-54-002.SDR CA130913008Tube · mismanufactured(CAN) TWO TUBE ASSEMBLIES, BOTH NEW FROM THE MFG, HAD AN INCORRECT BEND. THE BEND WAS OUT BY 90 DEGREES WHEN COMPARED TO THE TUBE INSTALLED IN THE ACFT. THE TUBE ASSY CONNECTS TO THE FREON CHARGING POINT.SDR GLBA2013091300309Actuator · failedPILOT REPORTED THAT THEY LOWERED GEAR HANDLE, LANDING GEAR RELAY CIRCUIT BREAKER TRIPPED, GEAR DID NOT MOVE, HYD POWER PACK DID NOT START AND LANDING GEAR HANDLE RED LIGHT DID NOT ILLUMINATE, MANUALLY EXTENDED GEAR, HANDLE RED LIGHT DID ILLUMINATED, GEAR DID
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